Beginning signomial solve.
Allowing negative dual variable(s) as small as -6.15045731359e-12.
Allowing negative dual variable(s) as small as -4.9365069324e-12.
Allowing negative dual variable(s) as small as -4.79576664839e-12.
Allowing negative dual variable(s) as small as -1.98581351016e-11.
Solving took 4 GP solves and 5.77 seconds.
Warning: Variable [Re_Mission/Cruise/FlightSegment.1/AircraftPerf.1/TailAero.3_(0,)] could cause inaccurate result because it is above upper bound. Solution is 1155331.2266 but bound is 1000000.0000
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.58249280136e-12.
Allowing negative dual variable(s) as small as -4.94278402929e-12.
Allowing negative dual variable(s) as small as -4.81657292176e-12.
Allowing negative dual variable(s) as small as -1.9690761608e-11.
Solving took 4 GP solves and 2.38 seconds.
Warning: Variable [Re_Mission/Cruise/FlightSegment.1/AircraftPerf.1/TailAero.3_(0,)] could cause inaccurate result because it is above upper bound. Solution is 1155331.2266 but bound is 1000000.0000
Allowing negative dual variable(s) as small as -1.60966517893e-11.
Allowing negative dual variable(s) as small as -6.12120770738e-12.
Allowing negative dual variable(s) as small as -1.16663623206e-11.
Allowing negative dual variable(s) as small as -6.60280163878e-12.
Allowing negative dual variable(s) as small as -6.61388999124e-12.
Allowing negative dual variable(s) as small as -1.10114630088e-11.
Allowing negative dual variable(s) as small as -1.16822725538e-11.
Allowing negative dual variable(s) as small as -1.10543824528e-11.
Allowing negative dual variable(s) as small as -1.11124146994e-11.
MTOW [lbs] = 141.59
Zero fuel weight [lbs] = 53.63
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.769
speed at top of climb [m/s] = 26.550
design loiter speed [m/s] = 25.056
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -1.79880444307e-11.
Allowing negative dual variable(s) as small as -6.27769971423e-12.
Allowing negative dual variable(s) as small as -1.04104867088e-11.
Allowing negative dual variable(s) as small as -1.04255732736e-11.
optimum loiter speed for min power, start of loiter [m/s] = 25.207
optimum loiter speed for min power, end of loiter [m/s] = 17.178
optimum cruise speed, inbound [m/s] = 36.034
optimum cruise speed, outbound [m/s] = 25.521
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.91636103326e-12.
Allowing negative dual variable(s) as small as -1.24251019352e-13.
Allowing negative dual variable(s) as small as -8.84840415321e-14.
Allowing negative dual variable(s) as small as -9.0769498313e-14.
Solving took 4 GP solves and 1.9 seconds.
Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1078212.3036 but bound is 1000000.0000
Max Speed [m/s]: 74.35
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.91010524511e-11.
Allowing negative dual variable(s) as small as -8.93119341504e-11.
Allowing negative dual variable(s) as small as -8.98729940295e-11.
Allowing negative dual variable(s) as small as -8.47845552446e-11.
Solving took 4 GP solves and 4.06 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -1.61376051411e-11.
Allowing negative dual variable(s) as small as -6.10016898106e-12.
Allowing negative dual variable(s) as small as -1.16599438438e-11.
Allowing negative dual variable(s) as small as -6.59762522393e-12.
Allowing negative dual variable(s) as small as -6.59297616501e-12.
Allowing negative dual variable(s) as small as -1.10139015963e-11.
Allowing negative dual variable(s) as small as -1.1686682763e-11.
Allowing negative dual variable(s) as small as -1.1052953908e-11.
Allowing negative dual variable(s) as small as -1.11101757135e-11.
MTOW [lbs] = 141.59
Zero fuel weight [lbs] = 53.63
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.769
speed at top of climb [m/s] = 26.550
design loiter speed [m/s] = 25.056
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -1.79900087882e-11.
Allowing negative dual variable(s) as small as -6.27464367357e-12.
Allowing negative dual variable(s) as small as -1.04054147026e-11.
Allowing negative dual variable(s) as small as -1.04263317815e-11.
optimum loiter speed for min power, start of loiter [m/s] = 25.207
optimum loiter speed for min power, end of loiter [m/s] = 17.178
optimum cruise speed, inbound [m/s] = 36.034
optimum cruise speed, outbound [m/s] = 25.521
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.91645060402e-12.
Allowing negative dual variable(s) as small as -1.2662445411e-13.
Allowing negative dual variable(s) as small as -8.83279135605e-14.
Allowing negative dual variable(s) as small as -9.08969135617e-14.
Solving took 4 GP solves and 2.1 seconds.
Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1078212.3036 but bound is 1000000.0000
Max Speed [m/s]: 74.35
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.91001464917e-11.
Allowing negative dual variable(s) as small as -8.93004697966e-11.
Allowing negative dual variable(s) as small as -8.9873163165e-11.
Allowing negative dual variable(s) as small as -8.47834966296e-11.
Solving took 4 GP solves and 5.57 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Passed

Standard Output

Standard Error
